NO913362L - Gassturbin for kraftproduksjon. - Google Patents

Gassturbin for kraftproduksjon.

Info

Publication number
NO913362L
NO913362L NO91913362A NO913362A NO913362L NO 913362 L NO913362 L NO 913362L NO 91913362 A NO91913362 A NO 91913362A NO 913362 A NO913362 A NO 913362A NO 913362 L NO913362 L NO 913362L
Authority
NO
Norway
Prior art keywords
gas turbine
power production
production
power
turbine
Prior art date
Application number
NO91913362A
Other languages
English (en)
Other versions
NO913362D0 (no
Inventor
Roy Marshall Washam
Jr Lewis Berkley Davis
Charles Evan Steber
Original Assignee
Gen Electric
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of NO913362D0 publication Critical patent/NO913362D0/no
Publication of NO913362L publication Critical patent/NO913362L/no

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36—Supply of different fuels

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
NO91913362A 1990-08-28 1991-08-27 Gassturbin for kraftproduksjon. NO913362L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/573,727 US5203796A (en) 1990-08-28 1990-08-28 Two stage v-gutter fuel injection mixer

Publications (2)

Publication Number Publication Date
NO913362D0 NO913362D0 (no) 1991-08-27
NO913362L true NO913362L (no) 1992-03-02

Family

ID=24293151

Family Applications (1)

Application Number Title Priority Date Filing Date
NO91913362A NO913362L (no) 1990-08-28 1991-08-27 Gassturbin for kraftproduksjon.

Country Status (5)

Country Link
US (1) US5203796A (no)
EP (1) EP0473371A1 (no)
JP (1) JPH04244511A (no)
KR (1) KR940001926B1 (no)
NO (1) NO913362L (no)

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FR2696502B1 (fr) * 1992-10-07 1994-11-04 Snecma Dispositif de post-combustion pour turbo réacteur double flux.
FR2706588B1 (fr) * 1993-06-16 1995-07-21 Snecma Système d'injection de carburant pour chambre de combustion.
US5927076A (en) * 1996-10-22 1999-07-27 Westinghouse Electric Corporation Multiple venturi ultra-low nox combustor
US5782079A (en) * 1997-02-25 1998-07-21 Industrial Technology Research Institute Miniature liquid-fueled turbojet engine
AU2341100A (en) * 1998-08-17 2000-04-17 Ramgen Power Systems, Inc. Apparatus and method for fuel-air mixing before supply of low pressure lean pre-mix to combustor
FR2835906B1 (fr) * 2002-02-13 2004-06-04 Saint Gobain Isover Bruleur a combustion interne, notamment pour l'etirage de fibres minerales
US7308793B2 (en) * 2005-01-07 2007-12-18 Power Systems Mfg., Llc Apparatus and method for reducing carbon monoxide emissions
US8671658B2 (en) * 2007-10-23 2014-03-18 Ener-Core Power, Inc. Oxidizing fuel
US20090111063A1 (en) * 2007-10-29 2009-04-30 General Electric Company Lean premixed, radial inflow, multi-annular staged nozzle, can-annular, dual-fuel combustor
US9822649B2 (en) * 2008-11-12 2017-11-21 General Electric Company Integrated combustor and stage 1 nozzle in a gas turbine and method
US8701413B2 (en) 2008-12-08 2014-04-22 Ener-Core Power, Inc. Oxidizing fuel in multiple operating modes
EP2208934A1 (en) * 2009-01-15 2010-07-21 ALSTOM Technology Ltd Burner of a gas turbine for a reactive fuel air mixture
US8616002B2 (en) * 2009-07-23 2013-12-31 General Electric Company Gas turbine premixing systems
US8763400B2 (en) * 2009-08-04 2014-07-01 General Electric Company Aerodynamic pylon fuel injector system for combustors
EP2496882B1 (en) 2009-11-07 2018-03-28 Ansaldo Energia Switzerland AG Reheat burner injection system with fuel lances
EP2496883B1 (en) 2009-11-07 2016-08-10 Alstom Technology Ltd Premixed burner for a gas turbine combustor
EP2496885B1 (en) 2009-11-07 2019-05-29 Ansaldo Energia Switzerland AG Burner with a cooling system allowing an increased gas turbine efficiency
WO2011054739A2 (en) * 2009-11-07 2011-05-12 Alstom Technology Ltd Reheat burner injection system
EP2496884B1 (en) 2009-11-07 2016-12-28 General Electric Technology GmbH Reheat burner injection system
US9027324B2 (en) * 2010-12-28 2015-05-12 Rolls-Royce North American Technologies, Inc. Engine and combustion system
US8863525B2 (en) 2011-01-03 2014-10-21 General Electric Company Combustor with fuel staggering for flame holding mitigation
US20120167578A1 (en) * 2011-01-04 2012-07-05 General Electric Company Flame holding inhibitor for a lean pre-nozzle fuel injection diffuser and related method
US8955329B2 (en) 2011-10-21 2015-02-17 General Electric Company Diffusion nozzles for low-oxygen fuel nozzle assembly and method
US11015808B2 (en) 2011-12-13 2021-05-25 General Electric Company Aerodynamically enhanced premixer with purge slots for reduced emissions
US9567903B2 (en) 2012-03-09 2017-02-14 Ener-Core Power, Inc. Gradual oxidation with heat transfer
US9726374B2 (en) 2012-03-09 2017-08-08 Ener-Core Power, Inc. Gradual oxidation with flue gas
US9534780B2 (en) 2012-03-09 2017-01-03 Ener-Core Power, Inc. Hybrid gradual oxidation
US9353946B2 (en) 2012-03-09 2016-05-31 Ener-Core Power, Inc. Gradual oxidation with heat transfer
US9359947B2 (en) 2012-03-09 2016-06-07 Ener-Core Power, Inc. Gradual oxidation with heat control
US9328660B2 (en) 2012-03-09 2016-05-03 Ener-Core Power, Inc. Gradual oxidation and multiple flow paths
US9347664B2 (en) 2012-03-09 2016-05-24 Ener-Core Power, Inc. Gradual oxidation with heat control
US9328916B2 (en) 2012-03-09 2016-05-03 Ener-Core Power, Inc. Gradual oxidation with heat control
US9371993B2 (en) 2012-03-09 2016-06-21 Ener-Core Power, Inc. Gradual oxidation below flameout temperature
US9381484B2 (en) 2012-03-09 2016-07-05 Ener-Core Power, Inc. Gradual oxidation with adiabatic temperature above flameout temperature
US9359948B2 (en) 2012-03-09 2016-06-07 Ener-Core Power, Inc. Gradual oxidation with heat control
US10094289B2 (en) * 2012-09-06 2018-10-09 United Technologies Corporation Cavity swirl fuel injector for an augmentor section of a gas turbine engine
CA2830031C (en) * 2012-10-23 2016-03-15 Alstom Technology Ltd. Burner for a can combustor
US10436117B2 (en) * 2013-01-18 2019-10-08 United Technologies Corporation Carbureted fuel injection system for a gas turbine engine
JP6206648B2 (ja) * 2013-07-08 2017-10-04 三菱日立パワーシステムズ株式会社 チップホルダ、これを備える燃焼器ノズル、この燃焼器ノズルを備える燃焼器、及び燃焼器ノズルの製造方法
CA2988555C (en) * 2015-06-16 2019-03-26 Ihi Corporation Engine aft section structure
US11149948B2 (en) 2017-08-21 2021-10-19 General Electric Company Fuel nozzle with angled main injection ports and radial main injection ports
WO2023033855A1 (en) * 2021-08-31 2023-03-09 Siemens Energy, Inc. Combustor having bluff bodies

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Publication number Priority date Publication date Assignee Title
US2632300A (en) * 1949-08-03 1953-03-24 Thermal Res & Engineering Corp Combustion stabilization means having igniter grill heated by pilotburner
US2771743A (en) * 1951-08-10 1956-11-27 Rolls Royce Gas-turbine engine with reheat combustion equipment
GB709452A (en) * 1951-10-16 1954-05-26 Napier & Son Ltd Improvements in or relating to liquid fuel combustion apparatus more particularly for gas turbine plant
US2948117A (en) * 1956-10-01 1960-08-09 Gen Electric Afterburner flameholder
US3018626A (en) * 1960-02-02 1962-01-30 Gen Electric Vapor combustion system
FR1321385A (fr) * 1962-05-09 1963-03-15 Rolls Royce Réchauffeur à combustion pour turbine à gaz ou analogue
US3176465A (en) * 1962-08-27 1965-04-06 Gen Electric Vapor fuel injector flameholder
FR1364192A (fr) * 1963-05-22 1964-06-19 Bristol Siddeley Engines Ltd Perfectionnements apportés aux moteurs de propulsion par réaction
US3153324A (en) * 1963-05-29 1964-10-20 Robert E Meyer Simplified primary fuel system
US3315468A (en) * 1965-10-01 1967-04-25 Gen Electric Cooled flameholder assembly
US3777983A (en) * 1971-12-16 1973-12-11 Gen Electric Gas cooled dual fuel air atomized fuel nozzle
JPS5026880B2 (no) * 1973-05-08 1975-09-03
US4445339A (en) * 1980-11-24 1984-05-01 General Electric Co. Wingtip vortex flame stabilizer for gas turbine combustor flame holder
GB2175993B (en) * 1985-06-07 1988-12-21 Rolls Royce Improvements in or relating to dual fuel injectors
US4893468A (en) * 1987-11-30 1990-01-16 General Electric Company Emissions control for gas turbine engine

Also Published As

Publication number Publication date
KR920020066A (ko) 1992-11-20
NO913362D0 (no) 1991-08-27
US5203796A (en) 1993-04-20
EP0473371A1 (en) 1992-03-04
KR940001926B1 (ko) 1994-03-11
JPH04244511A (ja) 1992-09-01

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